Effects of Sidewall Boundary Layers in Two-Dimensional Subsonic and Transonic Wind Tunnels
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference9 articles.
1. Similarity Rule for Sidewall Boundary Layer Effect in Two-Dimensional Wind Tunnels
2. Interactions between shock waves and turbulent boundary layers
3. 5Liepmann, H. W. and Rosko, A., Elements of Gas Dynamics, John Wiley & Sons, New York, 1957, pp.256-258.
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